A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft-Reference-Cited by-同舟云学术

A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Urnes James¹,Nguyen Nhan²

Affiliation:

1. The Boeing Company

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-214

Reference13 articles.

1. 2BoeingReportNo.2012X0015,“DevelopmentofVariableCamberContinuousTrailingEdgeFlapSystem,”October4,2012.

2. 3Jordan, T. L., Langford, W. M., Belcastro, C. M., Foster, J. M., Shah, G. H., Howland, G., and Kidd, R. “Development of a Dynamically ScaledGenericTransportModelTestbedforFlightResearchExperiments,”AUVSIUnmannedUnlimited,Arlington,VA,2004.

3. 5Nguyen,N.,Nelson,A.,andPulliam,T.“DamageAdaptiveControlSystemResearchReport,”InternalNASAReport,April2006.

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